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Forum: Main CFD Forum January 3, 2013, 09:20
Replies: 27
Views: 10,707
Posted By Far
For this purpose you need some reverse...

For this purpose you need some reverse engineering machines e.g. 3d scanner;)
Forum: Main CFD Forum November 1, 2011, 14:34
Replies: 27
Views: 10,707
Posted By Far
In my opinion you must try for the residual...

In my opinion you must try for the residual values at least 1e-6 for continuity, momentum, energy and turbulence quantities.
Forum: Main CFD Forum November 1, 2011, 14:30
Replies: 27
Views: 10,707
Posted By Far
1. which turbulence model you are using. 2. If...

1. which turbulence model you are using.
2. If you want to mesh in ICEM, I think you must go through blade pipe and wing body tutorial first. Creating mesh for centrifugal compressor is bit tricky....
Forum: Main CFD Forum October 28, 2011, 03:30
Replies: 27
Views: 10,707
Posted By Far
pls also attach the pic of convergence plot

pls also attach the pic of convergence plot
Forum: Main CFD Forum October 28, 2011, 03:29
Replies: 27
Views: 10,707
Posted By Far
Although it is not necessary to use the full...

Although it is not necessary to use the full structured grid for the turbomachinery or any other type of flows. But for turbomachinery flows, structured grid is used for the following reasons

1....
Forum: Main CFD Forum October 17, 2011, 12:39
Replies: 27
Views: 10,707
Posted By Far
you can mesh with gambit and gridgen easily. If...

you can mesh with gambit and gridgen easily. If needed I can show you method on my computer with the help of skype.
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